Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"

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<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
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|file=J33WheesleyBasicJetEngine.png
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|type=je
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|size=s
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|manufacturer=C7
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|costs=950
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|mass=1.5
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|drag=0.2
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|temp=2000
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|tolerance=7
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|research=Aerodynamics
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|unlock cost=4000
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|since=0.15
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|filename=jetEngineBasic.cfg
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|part=jetEngineBasic
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|more=
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{{Infobox/Part/jet engine
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|isp=9600
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|thrust=120
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|vectoring=
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}}
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{{Infobox/Part/test subject
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|environments=71
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|event=True
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|staging=True
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}}
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}}

Revision as of 18:48, 17 March 2017

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
J-33 "Wheesley" Turbofan Engine
Part image
Jet engine by
C7 Aerospace Division

Radial size Small
Cost (total) 950.00 Funds
Mass (total) 1.500 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 4 000 Funds
Since version 0.15
Part configuration jetEngineBasic.cfg
Maximum thrust 120.00 kN
Isp (max) 9600 s
Fuel consumption 0.25 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring No
Testing Environments
On the surface Yes
In the ocean Yes
On the launchpad Yes
In the atmosphere No
Sub-orbital No
In an orbit No
On an escape Yes
Docked No
Test by staging Yes
Manually testable Yes